Has JWST done its first station keeping yet? The last burn I know about was the MCC2 burn on Jan24; more than 21 days ago; and that was a pretty long burn with a $\Delta v$ of 1.6 m/sec or 160 cm/sec, which is much larger than the 12cm/sec minimal so I would assume they would want another burn at 21 days just because JWST must always stay on the Earth side of the halo orbit, and there had to be some reasonable margin in the MCC2 burn.
This question is somewhat inspired by uhoh's answer to How frequent are (or will be) JWST station keeping burns at L2? which quotes the Monte Carlo Paper:
Stationkeeping (SK) maneuvers will be performed every 21 days to keep JWST in an LPO around the unstable SEM L2 point... a planned maneuver that would be smaller than 12 cm/sec would be skipped for efficiency... so in most cases an SK maneuver would be performed every 42 days, not every 21 days.
A second somewhat related question is how close does JWST get to the top of the hill/saddle, from which JWST would escape, including the solar radiation? The closer JWST is to the saddle, the less fuel is used for station keeping, but JWST must always stay on the Earth side of the saddle since the station keeping engines only fire in one direction, towards the sun.
For the 2nd half of the question, take JWST's current position and velocity, and only change the distance to the sun. The if JWST is a few hundred kilometers further from the sun, or at most a few thousand kilometers early in the project, then JWST is on the wrong side of the saddle and will irrevocably escape Earth's pull and go into orbit around the sun instead.
JWST
for the target, and@32
(which is the Sun-EMB L2 point) for the center. $\endgroup$